FR Turbojet T70
Compact and cost-effective
Weight (core engine)
7.5 kg
Max thrust
750 N
Combustion test cell
Small, low-cost turbojet engine capable of generating 750 N of maximum thrust. Capable of high-altitude startup and of windmilling start
Specific Fuel Consumption
0.108 kg/h/N
Electrical power output
up to 2000 W
Length
360 mm
Outer diameter
170 mm
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